Deformation analysis of wing structures

The elementary theories of bending and torsion often do not describe the stresses in aircraft shell structures with adequate accuracy; more refined stress theories have therefore have developed over a period of years. Theories of this nature are applied to the problem of calculating the deflections,...

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Bibliographic Details
Main Author: Kuhn, Paul, (Author)
Corporate Author: Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1361.
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ISBN: 9781680156072
1680156071
Physical Description: 1 online resource (34 pages, 9 unnumbered pages) : illustrations

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